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Received: 2003-04-21

Revision Accepted: 2003-07-10

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Journal of Zhejiang University SCIENCE A 2004 Vol.5 No.5 P.609-617


Nonlinear dynamic buckling of stiffened plates under in-plane impact load

Author(s):  ZHANG Tao, LIU Tu-guang, ZHAO Yao, LUO Jia-zhi

Affiliation(s):  College of Traffic and Engineering, Huazhong University of Science and Technology, Wuhan 430074, China

Corresponding email(s):   icesheet@public.wh.hb.cn

Key Words:  Stiffened plate, Dynamic buckling, In-plane impact

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ZHANG Tao, LIU Tu-guang, ZHAO Yao, LUO Jia-zhi. Nonlinear dynamic buckling of stiffened plates under in-plane impact load[J]. Journal of Zhejiang University Science A, 2004, 5(5): 609-617.

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T1 - Nonlinear dynamic buckling of stiffened plates under in-plane impact load
A1 - ZHANG Tao
A1 - LIU Tu-guang
A1 - ZHAO Yao
A1 - LUO Jia-zhi
J0 - Journal of Zhejiang University Science A
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DOI - 10.1631/jzus.2004.0609

This paper presents a simple solution of the dynamic buckling of stiffened plates under in-plane impact loading. Based on large deflection theory, a discretely stiffened plate model has been used. The tangential stresses of stiffeners and in-plane displacement are neglected. Appling the Hamilton's principle, the motion equations of stiffened plates are obtained. The deflection of the plate is taken as Fourier series, and using Galerkin method the discrete equations can be deduced, which can be solved easily by Runge-Kutta method. The dynamic buckling loads of the stiffened plates are obtained form Budiansky-Roth criterion.

Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article


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2014-11-22 17:33:37

Many thanks


2014-07-20 23:09:35

thank you for paper


2014-03-22 17:00:50

i want this paper

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